US7725210B2 - Method of processing turbine components - Google Patents

Method of processing turbine components Download PDF

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Publication number
US7725210B2
US7725210B2 US11/734,352 US73435207A US7725210B2 US 7725210 B2 US7725210 B2 US 7725210B2 US 73435207 A US73435207 A US 73435207A US 7725210 B2 US7725210 B2 US 7725210B2
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United States
Prior art keywords
laser
coating
recited
turbine component
cooling
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US11/734,352
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English (en)
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US20070241084A1 (en
Inventor
Matthias Hoebel
Bernd Fehrmann
Christoph Kohles
Karsten Franitza
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General Electric Technology GmbH
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Alstom Technology AG
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Assigned to ALSTOM TECHNOLOGY LTD reassignment ALSTOM TECHNOLOGY LTD ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: FRANITZA, KARSTEN, KOHLES, CHRISTOPH, FEHRMANN, BERND, HOEBEL, MATTHIAS
Publication of US20070241084A1 publication Critical patent/US20070241084A1/en
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Assigned to GENERAL ELECTRIC TECHNOLOGY GMBH reassignment GENERAL ELECTRIC TECHNOLOGY GMBH CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: ALSTOM TECHNOLOGY LTD
Assigned to ANSALDO ENERGIA IP UK LIMITED reassignment ANSALDO ENERGIA IP UK LIMITED ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GENERAL ELECTRIC TECHNOLOGY GMBH
Assigned to GENERAL ELECTRIC TECHNOLOGY GMBH reassignment GENERAL ELECTRIC TECHNOLOGY GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ANSALDO ENERGIA IP UK LIMITED
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005Repairing methods or devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/38Removing material by boring or cutting
    • B23K26/382Removing material by boring or cutting by boring
    • B23K26/389Removing material by boring or cutting by boring of fluid openings, e.g. nozzles, jets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/001Turbines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/06Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/10Manufacture by removing material
    • F05D2230/13Manufacture by removing material using lasers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/90Coating; Surface treatment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611Coating
US11/734,352 2006-04-13 2007-04-12 Method of processing turbine components Active 2028-03-22 US7725210B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP06112639A EP1844892A1 (de) 2006-04-13 2006-04-13 Verfahren zur Laserentfernung von Beschichtenmaterialen in Kühlenlöchern eines Turbinenbauteiles
EP06112639.7 2006-04-13
EP06112639 2006-04-13

Publications (2)

Publication Number Publication Date
US20070241084A1 US20070241084A1 (en) 2007-10-18
US7725210B2 true US7725210B2 (en) 2010-05-25

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Family Applications (1)

Application Number Title Priority Date Filing Date
US11/734,352 Active 2028-03-22 US7725210B2 (en) 2006-04-13 2007-04-12 Method of processing turbine components

Country Status (3)

Country Link
US (1) US7725210B2 (de)
EP (2) EP1844892A1 (de)
DE (1) DE502007000800D1 (de)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012122432A (ja) * 2010-12-10 2012-06-28 Mitsubishi Heavy Ind Ltd コーティング部材の孔位置特定装置
US20120164376A1 (en) * 2010-12-23 2012-06-28 General Electric Company Method of modifying a substrate for passage hole formation therein, and related articles
US20140273747A1 (en) * 2013-03-15 2014-09-18 United Technologies Corporation Removing material from a workpiece with a water jet
US9348001B2 (en) 2013-10-21 2016-05-24 General Electric Company Method and system for detecting surface features on turbine components
US20160193693A1 (en) * 2014-02-28 2016-07-07 Mitsubishi Heavy Industries, Ltd. Laser processing method and laser processing apparatus
US9707645B2 (en) 2014-01-09 2017-07-18 General Electric Company Systems, methods, and apparatus for locating and drilling closed holes of a turbine component
US20190039177A1 (en) * 2017-08-07 2019-02-07 United Technologies Corporation Laser clearance of coating
US20210130946A1 (en) * 2018-07-09 2021-05-06 Siemens Aktiengesellschaft Device and method for removing coating material from openings in a part
EP3936278A1 (de) * 2020-07-06 2022-01-12 Pratt & Whitney Canada Corp. Verfahren zur reparatur einer brennkammerauskleidung eines gasturbinenmotors
US11407067B2 (en) * 2018-06-29 2022-08-09 Pratt & Whitney Canada Corp. Method for repairing a part
US11953309B2 (en) 2021-09-22 2024-04-09 Lockheed Martin Corporation Automated non-contact thickness inspection and projection system using color-coded based patterns

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US8319146B2 (en) * 2009-05-05 2012-11-27 General Electric Company Method and apparatus for laser cutting a trench
EP2312122A1 (de) * 2009-10-15 2011-04-20 Siemens Aktiengesellschaft Referenzbestimmung zur Ermittlung der Lage von verschlossenen Löchern, Vorrichtung und Bearbeitungsvorrichtung
EP2312267A1 (de) * 2009-10-19 2011-04-20 Siemens Aktiengesellschaft Verfahren zur Schichtdickenmessung mittels Lasertriangulation und Vorrichtung
EP2385214A1 (de) * 2010-05-06 2011-11-09 Siemens Aktiengesellschaft Verfahren zur Ermittlung der Lage von verschlossenen Löchern, Vorrichtung und Bearbeitungsvorrichtung
EP2386824A1 (de) * 2010-05-12 2011-11-16 Siemens Aktiengesellschaft Oberflächenanalyse zur Detektierung veschlossener Löcher und Verfahren zur Wiederöffnung
EP2386823A1 (de) * 2010-05-12 2011-11-16 Siemens Aktiengesellschaft Oberflächenanalyse zur Detektierung verschlossener Löcher und Verfahren zur Wiedereröffnung
EP2508844A1 (de) * 2011-04-08 2012-10-10 Siemens Aktiengesellschaft Verfahren zum Bestimmen einer Beschichtungsdicke
US9434025B2 (en) 2011-07-19 2016-09-06 Pratt & Whitney Canada Corp. Laser drilling methods of shallow-angled holes
US20130020291A1 (en) * 2011-07-19 2013-01-24 Pratt & Whitney Canada Corp. Laser drilling methods of shallow-angled holes
EP2604378B1 (de) * 2011-12-15 2015-04-01 Siemens Aktiengesellschaft Wiederöffnung von Kühlluftbohrungen mit Nanosekundenlaser im Mikrosekundenbereich
EP2716788A1 (de) * 2012-10-08 2014-04-09 Siemens Aktiengesellschaft Verfahren zum Entfernen einer metallischen Schicht von einem Substrat
WO2014151479A2 (en) * 2013-03-22 2014-09-25 Videojet Technologies Inc. Method of removing a coating of a substrate
DE102013211047B4 (de) * 2013-06-13 2015-04-30 MTU Aero Engines AG Verfahren zum Verschließen von Kühlluftbohrungen
US20150160644A1 (en) * 2013-12-05 2015-06-11 General Electric Company Repair method, system for automatic locating and clearing and tool for automated locating and modifying
DE102014204806A1 (de) 2014-03-14 2015-09-17 Siemens Aktiengesellschaft Verfahren zur Neuherstellung von Durchgangslöchern in einem Schichtsystem
CN104036085B (zh) * 2014-06-18 2017-03-15 无锡吉兴汽车声学部件科技有限公司 用于cae仿真分析的复杂型面汽车声学部件的厚度统计方法
US10101030B2 (en) * 2014-09-02 2018-10-16 Honeywell International Inc. Gas turbine engines with plug resistant effusion cooling holes
US20160214208A1 (en) * 2015-01-22 2016-07-28 General Electric Company System and method for forming passages in an airfoil
US20160243655A1 (en) * 2015-02-20 2016-08-25 General Electric Company Component repair using confined laser drilling
CN105728956B (zh) * 2016-05-09 2017-07-04 环维电子(上海)有限公司 一种sip模组的镭射切割方法及系统
US11813706B2 (en) * 2021-08-13 2023-11-14 Rtx Corporation Methods for forming cooling apertures in a turbine engine component

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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012122432A (ja) * 2010-12-10 2012-06-28 Mitsubishi Heavy Ind Ltd コーティング部材の孔位置特定装置
US20120164376A1 (en) * 2010-12-23 2012-06-28 General Electric Company Method of modifying a substrate for passage hole formation therein, and related articles
US20140273747A1 (en) * 2013-03-15 2014-09-18 United Technologies Corporation Removing material from a workpiece with a water jet
US9403259B2 (en) * 2013-03-15 2016-08-02 United Technologies Corporation Removing material from a workpiece with a water jet
US9348001B2 (en) 2013-10-21 2016-05-24 General Electric Company Method and system for detecting surface features on turbine components
US9707645B2 (en) 2014-01-09 2017-07-18 General Electric Company Systems, methods, and apparatus for locating and drilling closed holes of a turbine component
US10792759B2 (en) * 2014-02-28 2020-10-06 Mitsubishi Heavy Industries, Ltd. Laser processing method and laser processing apparatus
US20160193693A1 (en) * 2014-02-28 2016-07-07 Mitsubishi Heavy Industries, Ltd. Laser processing method and laser processing apparatus
US20190039177A1 (en) * 2017-08-07 2019-02-07 United Technologies Corporation Laser clearance of coating
US11752573B2 (en) * 2017-08-07 2023-09-12 Rtx Corporation Laser clearance of coating
US11407067B2 (en) * 2018-06-29 2022-08-09 Pratt & Whitney Canada Corp. Method for repairing a part
US20210130946A1 (en) * 2018-07-09 2021-05-06 Siemens Aktiengesellschaft Device and method for removing coating material from openings in a part
US11898237B2 (en) * 2018-07-09 2024-02-13 Siemens Energy Global GmbH & Co. KG Device and method for removing coating material from openings in a part
EP3936278A1 (de) * 2020-07-06 2022-01-12 Pratt & Whitney Canada Corp. Verfahren zur reparatur einer brennkammerauskleidung eines gasturbinenmotors
US11840032B2 (en) 2020-07-06 2023-12-12 Pratt & Whitney Canada Corp. Method of repairing a combustor liner of a gas turbine engine
US11953309B2 (en) 2021-09-22 2024-04-09 Lockheed Martin Corporation Automated non-contact thickness inspection and projection system using color-coded based patterns

Also Published As

Publication number Publication date
DE502007000800D1 (de) 2009-07-16
EP1844893A1 (de) 2007-10-17
US20070241084A1 (en) 2007-10-18
EP1844893B1 (de) 2009-06-03
EP1844892A1 (de) 2007-10-17

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